Learjet 24

Learjet · United States · first flew 1966 · light aircraft

The Learjet 24 is a six-to-eight-seat, twin-engined, high-speed business jet built by Learjet as the successor to the Learjet 23.

Recognition (WEFT)

W — WingsLow-mounted, swept
E — Engines2 × turbojet, fuselage-mounted
F — FuselageTwo rear-fuselage turbojets, in the pattern of the Learjet 23
T — TailConventional

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Spot it by:

A small low-wing jet with wingtip tanks and rear-mounted engines; the 24D and later have rectangular cabin windows where the earlier models have round ones.

Specifications

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

It was designed to take the full 13,500 lb weight permitted by FAR-25, with more powerful engines, a new windshield, wingtip tanks and an engine fire-extinguishing system. It first flew on 24 January 1966 and became the first business jet certified under FAR-25.

Variants

Variants were the 24A, 24B, 24C (not built), 24D, 24E and 24F. The 24D replaced the round cabin windows with angular ones, and the 24E and 24F introduced a cambered wing.

Where you'll see it

259 were built between 1966 and 1977. A Learjet 24 flew around the world in 50 hours 20 minutes of flying time in May 1966, and NASA used one as the Learjet Observatory.

Related aircraft

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